Fire extinguishing bomb throwing unmanned aerial vehicle

By designing a fire extinguishing bomb delivery drone, which utilizes an electric motor to drive the blades and a cylinder spring to control the release assembly, the limitations of traditional fire extinguishing methods in large-scale fires have been overcome, improving fire extinguishing efficiency and safety, and protecting the safety of firefighters.

CN223559844UActive Publication Date: 2025-11-18YIFEI GALAXY (TIANJIN) INTELLIGENT TECH CO LTD
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Patent Information

Application Number
CN202423303761.2
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-12-31
Publication Date
2025-11-18
Estimated Expiration
2034-12-31

AI Technical Summary

Technical Problem

Traditional manual firefighting methods, such as ground fire brigades and helicopter water drop, have problems such as slow response speed, limited coverage, great restriction by terrain and weather conditions, and threats to personnel safety when facing large-scale and rapidly spreading fires.

Method used

Design a fire extinguishing bomb delivery drone that uses motor-driven blades for flight and is equipped with a delivery mechanism, including a housing, sleeve, cross plate, and release assembly. The release of the fire extinguishing bomb is controlled by a connecting assembly consisting of a cylinder and a spring, ensuring that the fire extinguishing bomb is delivered at a predetermined time.

Benefits of technology

It improved the efficiency of firefighting operations, reduced the possibility of personnel directly participating in high-risk tasks, enhanced the reliability and response speed of the system, and protected the safety of firefighters.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a fire extinguishing bomb throwing unmanned aerial vehicle, which belongs to the technical field of unmanned aerial vehicles and comprises a support. The motor is fixedly connected to the upper end of the support, and the output end of the motor is fixedly connected with blades; the bottom plate is fixedly connected to the lower end of the bracket; the throwing mechanism comprises a box body, four sleeves, two transverse plates, fire extinguishing bombs and a releasing assembly, the box body is in threaded connection to the lower end of the bottom plate through bolts, the four sleeves are fixedly connected into the box body, the two transverse plates are fixedly connected between the sleeves and the box body, the fire extinguishing bombs are arranged in the four sleeves respectively, and the releasing assembly is arranged in the box body. The releasing part is arranged at the lower end of the box body to realize throwing of the fire extinguishing bomb; the unmanned aerial vehicle is specially designed for throwing the fire extinguishing bombs and can release the fire extinguishing bombs above a fire scene. Autonomous flight is realized by using blades driven by a motor, and a designed throwing mechanism is arranged, so that the fire extinguishing bomb can be thrown to a target position.
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Description

TECHNICAL FIELD

[0001] The utility model belongs to unmanned plane technical field, concretely relates to a fire extinguishing bomb delivery unmanned plane. BACKGROUND

[0002] With the influence of global climate change and human activities, the frequency and intensity of fires, especially forest fires, have increased.

[0003] Traditional manual fire extinguishing methods such as ground fire brigade and helicopter water spraying have many limitations when facing large-area, rapidly spreading fires, such as slow response speed, limited coverage, greater restrictions on terrain and weather conditions, and threats to personnel safety. SUMMARY

[0004] The utility model aims at providing a fire extinguishing bomb delivery unmanned plane to solve the problems of traditional manual fire extinguishing methods such as ground fire brigade and helicopter water spraying in the prior art, such as slow response speed, limited coverage, greater restrictions on terrain and weather conditions, and threats to personnel safety.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical scheme:

[0006] A fire extinguishing bomb delivery unmanned plane comprises:

[0007] a support;

[0008] a motor fixedly connected to the upper end of the support, the output end of the motor being fixedly connected with a blade;

[0009] a bottom plate fixedly connected to the lower end of the support;

[0010] a delivery mechanism comprising a box, four sleeves, two cross plates, fire extinguishing bombs, and a release assembly, the box being threadedly connected to the lower end of the bottom plate, the four sleeves being fixedly connected inside the box, the two cross plates being fixedly connected between the sleeves and the box, the fire extinguishing bombs being arranged in the four sleeves, and the release assembly being arranged at the lower end of the box to realize the delivery of the fire extinguishing bombs.

[0011] As a preferred scheme of the utility model, the release assembly comprises a mounting seat, a closure plate, and a connecting assembly, the mounting seat being fixedly connected to the lower end of the box, the closure plate being connected to the lower end of the box, the mounting seat and the closure plate being rotationally connected through a rotating shaft, the protective pad being fixedly connected to the upper end of the closure plate, and the connecting assembly being arranged at the side end of the box to realize the opening of the closure plate.

[0012] As a preferred scheme of the utility model, the connecting assembly includes a cylinder, a connecting seat and a spring, the cylinder is fixedly connected to the side end of the box body, the connecting seat is fixedly connected to the side end of the closing plate, the output end of the cylinder is connected with the connecting seat, and the spring is connected between the connecting seat and the cylinder.

[0013] As a preferred scheme of the utility model, the upper end of the closing plate is fixedly connected with a protective pad, and the protective pad is matched with the fire extinguishing bomb.

[0014] As a preferred scheme of the utility model, the outer diameter of the protective pad is equal to the inner diameter of the sleeve.

[0015] As a preferred scheme of the utility model, the upper end of the support is fixedly connected with a connecting frame, and the upper end of the connecting frame is provided with a battery.

[0016] Compared with the prior art, the utility model has the beneficial effects that:

[0017] 1、In the scheme, the unmanned aerial vehicle is designed for launching fire extinguishing bombs, which can release fire extinguishing bombs above the fire scene. The use of motor-driven blades realizes autonomous flight, and the designed launching mechanism ensures that the fire extinguishing bomb can be delivered to the target position. This unmanned operation not only improves the efficiency of fire extinguishing operation, but also greatly reduces the possibility of personnel directly participating in high-risk fire extinguishing tasks, thereby protecting the safety of firefighters.

[0018] 2、In the scheme, the fire extinguishing bomb is safely placed in the sleeve, and the release of the fire extinguishing bomb is managed by the closing plate with the protective pad and the connecting assembly controlled by the cylinder. The design of the protective pad ensures the stability and integrity of the fire extinguishing bomb during transportation, preventing accidental triggering due to collision or vibration. The connecting assembly composed of the cylinder and the spring provides a quick and controllable release method, so that the fire extinguishing bomb can be launched at a predetermined time point, increasing the reliability and response speed of the entire system. BRIEF DESCRIPTION OF DRAWINGS

[0019] The accompanying drawings are used to provide a further understanding of the utility model, and constitute a part of the specification, together with the embodiments of the utility model, for explaining the utility model, and do not constitute a limitation on the utility model. In the drawings:

[0020] Figure 1 It is the first perspective view of the utility model;

[0021] Figure 2 It is the utility model

[0022] Figure 3 It is the utility model Figure 2 the explosion view of the box body;

[0023] Figure 4 For the utility model Figure 3 The explosion view at the middle box body.

[0024] In the drawing: 1, support; 2, motor; 3, blade; 4, connecting frame; 5, bottom plate; 6, box body; 7, air cylinder; 8, mounting seat; 9, closing plate; 10, protective pad; 11, connecting seat; 12, spring; 13, sleeve; 14, cross plate; 15, fire extinguishing bomb; 16, battery. DETAILED DESCRIPTION

[0025] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the utility model.

[0026] Embodiment 1

[0027] Please refer to Figures 1-4 The utility model provides the following technical scheme:

[0028] A fire extinguishing bomb launching unmanned aerial vehicle, comprising:

[0029] Support 1;

[0030] Motor 2, the upper end of support 1 is fixedly connected with motor 2, and the output end of motor 2 is fixedly connected with blade 3;

[0031] Bottom plate 5, the lower end of support 1 is fixedly connected with bottom plate 5;

[0032] Launching mechanism, the launching mechanism includes box body 6, four sleeves 13, two cross plates 14, fire extinguishing bomb 15 and release component, the lower end of bottom plate 5 is connected with box body 6 by bolt thread, four sleeves 13 are all fixedly connected in box body 6, two cross plates 14 are respectively fixedly connected between sleeve 13 and box body 6, fire extinguishing bomb 15 is respectively arranged in four sleeves 13, and release component is arranged at the lower end of box body 6 to realize the launching of fire extinguishing bomb 15.

[0033] In the specific embodiment of the utility model, the support 1 is the main structure of the whole unmanned aerial vehicle, providing the function of supporting and connecting other components. The motor 2 provides power for the unmanned aerial vehicle, driving the blade to rotate, so that the unmanned aerial vehicle can fly. The blade 3 is driven to rotate by the motor, generating lift to lift the unmanned aerial vehicle, and controlling the attitude and movement direction of the unmanned aerial vehicle by changing the rotation speed or angle. The bottom plate 5 is located below the support, mainly used for supporting and protecting the internal device, and also serving as the mounting platform of the box 6 and other lower components. The box 6 is used as a container for loading fire extinguishing bombs, and is also part of the release mechanism. It is fixed to the bottom plate by bolts, ensuring safety and stability during air transportation. The four sleeves 13 are used to contain and position the fire extinguishing bombs 15. They ensure that the fire extinguishing bombs do not move randomly during transportation, thereby ensuring safety. The two cross plates 14 are connected between the sleeves and the box, playing a role in strengthening the structural strength, and may also participate in limiting the position of the fire extinguishing bombs. The fire extinguishing bomb 15 is the key load of the unmanned aerial vehicle for executing tasks, used for extinguishing fires. The release component is arranged at the lower end of the box, responsible for opening the closure plate according to the preset conditions or remote instructions, so that the fire extinguishing bomb can be smoothly thrown out of the unmanned aerial vehicle.

[0034] For details, please refer to Figures 1-4 The release component includes a mounting seat 8, a closure plate 9 and a connecting assembly. The mounting seat 8 is fixedly connected to the lower end of the box 6, the closure plate 9 is connected to the lower end of the box 6, the mounting seat 8 and the closure plate 9 are rotationally connected through a rotating shaft, a protective pad 10 is fixedly connected to the upper end of the closure plate 9, and the connecting assembly is arranged at the side end of the box 6 to realize the opening of the closure plate 9.

[0035] In this embodiment: the mounting seat 8 serves as the fulcrum of the rotation of the closure plate 9. It provides stable connection between the closure plate and the box, and ensures that the closure plate can rotate smoothly around the rotating shaft to realize the opening and closing actions. The closure plate 9 functions to seal the box when the unmanned aerial vehicle carries the fire extinguishing bomb to fly, preventing the external environment from affecting the internal fire extinguishing bomb. When it is necessary to release the fire extinguishing bomb, the closure plate rotates around the rotating shaft to open, allowing the fire extinguishing bomb to fall smoothly from the box. The protective pad 10 directly contacts the fire extinguishing bomb. The main function of the protective pad is to protect the fire extinguishing bomb from damage, especially to provide a cushioning effect when the unmanned aerial vehicle takes off or encounters bumps; at the same time, it can also reduce the friction or collision between the closure plate and the fire extinguishing bomb, ensuring the safety of the fire extinguishing bomb. The connecting assembly is used to control the opening action of the closure plate 9.

[0036] For details, please refer to Figures 1-4 The connecting assembly includes a gas cylinder 7, a connecting seat 11 and a spring 12. The gas cylinder 7 is fixedly connected to the side end of the box 6, the connecting seat 11 is fixedly connected to the side end of the closure plate 9, the output end of the gas cylinder 7 is connected to the connecting seat 11, and the spring 12 is connected between the connecting seat 11 and the gas cylinder 7.

[0037] In this embodiment: the cylinder 7 is the main power source of the connecting assembly. It generates linear motion through internal pressure changes, usually gas or hydraulic, to drive the opening action of the closure plate 9. The output end of the cylinder is connected to the connecting seat 11, when the cylinder extends or retracts, it will drive the closure plate to rotate around the rotating shaft, so as to realize the opening or closing of the closure plate. The connecting seat 11 serves as a connecting bridge between the cylinder 7 and the closure plate. It transmits the force from the cylinder to the closure plate, so that the closure plate can move in the expected way. In addition, the connecting seat also provides a fixed mounting point for the spring 12, so that the spring can maintain appropriate tension when the cylinder retracts, and assist the closure plate to reset when needed. The spring 12 plays a role in buffering and assisting reset. When the cylinder pushes the closure plate to open, the spring will be stretched; in the case of cylinder retraction or loss of pressure, the spring can help the closure plate quickly return to the closed position.

[0038] For details, please refer to Figures 1-4 The upper end of the closure plate 9 is fixedly connected with a protective pad 10, which is matched with the fire extinguishing bomb 15.

[0039] In this embodiment: the main function of the protective pad 10 is to provide cushioning between the fire extinguishing bomb and the closure plate, preventing damage to the fire extinguishing bomb caused by vibration or impact during the take-off and landing of the unmanned aerial vehicle or during flight. Especially when the unmanned aerial vehicle encounters air turbulence or lands, the protective pad can effectively absorb the impact force and ensure the integrity of the fire extinguishing bomb.

[0040] For details, please refer to Figures 1-4 The outer diameter of the protective pad 10 is equal to the inner diameter of the sleeve 13.

[0041] In this embodiment: since the outer diameter of the protective pad 10 is completely matched with the inner diameter of the sleeve 13, this design can ensure the positioning of the fire extinguishing bomb inside the sleeve 13. This can prevent unnecessary movement or rotation of the fire extinguishing bomb during transportation, maintain its stable position, and thus ensure the accuracy and consistency of the release. The equal outer diameter and inner diameter size means that there is almost no gap between the protective pad 10 and the sleeve 13, which helps to form a relatively closed space. If the unmanned aerial vehicle encounters changes in air flow or air pressure during flight, the close fit can help reduce the influence of the external environment on the fire extinguishing bomb, such as dust, moisture or other contaminants entering the inside of the sleeve.

[0042] For details, please refer to Figures 1-4 The upper end of the bracket 1 is fixedly connected with a connecting frame 4, and the upper end of the connecting frame 4 is provided with a battery 16.

[0043] In this embodiment: the bracket 1 is the basic structure of the entire unmanned aerial vehicle, which provides stable support for all components mounted thereon. By fixing the connecting frame 4 to the upper end of the bracket, the stability of the connecting frame and the battery 16 above it is ensured, even when encountering bumps or airflow changes during flight, wherein the battery 16 is the power source of the unmanned aerial vehicle, located at the upper end of the connecting frame 4, which can provide a centralized power supply point for the unmanned aerial vehicle.

[0044] The working principle and use process of the utility model: first, the operator issues a take-off instruction when in use, the unmanned aerial vehicle ascends according to the predetermined route, and the unmanned aerial vehicle automatically navigates to the specified target area according to the GPS and other navigation equipment, maintains stable flight in the process, avoids unnecessary bumps affecting internal equipment, when the unmanned aerial vehicle reaches the predetermined drop point, the system will automatically activate the release assembly according to the preset conditions such as geographical coordinates, time or other trigger factors, the cylinder 7 receives the instruction and starts to act, pushes the connecting seat 11, makes the closing plate 9 rotate around the rotating shaft and opens, the spring 12 assists this process, ensures that the closing plate can be opened smoothly and quickly, with the opening of the closing plate, the fire extinguishing bomb 15 slides out of the sleeve 13 and is thrown to the ground target, after all the predetermined fire extinguishing bombs are dropped, the unmanned aerial vehicle will return to the base according to the return route.

[0045] Finally, it should be noted that: the above only for the preferred embodiments of the utility model, and not for limiting the utility model, although the utility model has been described in detail with reference to the foregoing embodiments, for those skilled in the art, it still can modify the technical scheme recorded in the foregoing embodiments, or make equivalent replacement to part of the technical features. Any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the utility model should be included in the protection scope of the utility model.

Claims

1. A fire extinguishing bomb launching drone, characterized in that, Include: Support (1); Motor (2), the motor (2) is fixedly connected to the upper end of the support (1), and the output end of the motor (2) is fixedly connected with the blade (3); Bottom plate (5), the bottom plate (5) is fixedly connected to the lower end of the support (1); The release component includes a mounting seat (8), a closing plate (9) and a connecting assembly, the mounting seat (8) is fixedly connected to the lower end of the box body (6), the closing plate (9) is connected to the lower end of the box body (6), the mounting seat (8) and the closing plate (9) are rotatably connected through the rotating shaft, the protective pad (10) is fixedly connected to the upper end of the closing plate (9), and the connecting assembly is arranged on the side end of the box body (6) to realize the opening of the closing plate (9).

2. The fire extinguishing bomb launching drone according to claim 1, wherein: The connecting assembly includes a gas cylinder (7), a connecting seat (11) and a spring (12), the gas cylinder (7) is fixedly connected to the side end of the box body (6), the connecting seat (11) is fixedly connected to the side end of the closing plate (9), the output end of the gas cylinder (7) is connected with the connecting seat (11), and the spring (12) is connected between the connecting seat (11) and the gas cylinder (7).

3. The fire extinguishing bomb launching drone according to claim 2, wherein: The upper end of the closing plate (9) is fixedly connected with the protective pad (10), and the protective pad (10) is matched with the fire extinguishing bomb (15).

4. The fire extinguishing bomb launching drone according to claim 3, wherein: The outer diameter of the protective pad (10) is equal to the inner diameter of the sleeve (13).

5. The fire extinguishing bomb launching drone according to claim 4, wherein: The upper end of the support (1) is fixedly connected with the connecting frame (4), and the upper end of the connecting frame (4) is provided with the battery (16).

6. The fire extinguishing bomb launching drone according to claim 5, wherein: ​